N55000

Substantial
None

MAULE M 7-260CS/N: 30031C

Accident Details

Date
Tuesday, March 10, 2015
NTSB Number
CEN15LA170
Location
Oregon, MO
Event ID
20150312X61444
Coordinates
39.986946, -95.144996
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Engine vibration for reasons that could not be determined based on the available evidence.

Aircraft Information

Registration
Make
MAULE
Serial Number
30031C
Engine Type
Reciprocating
Year Built
2003
Model / ICAO
M 7-260C
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
5
FAA Model
M-7-260C

Registered Owner (Current)

Name
GROSS FLYING SERVICE INC
Address
PO BOX 393
City
LARNED
State / Zip Code
KS 67550-0393
Country
United States

Analysis

On March 10, 2015, about 1210 central daylight time, a Maule M7 airplane, N55000, sustained substantial damage when it nosed over during a precautionary landing near Oregon, Missouri, following a partial loss of engine power during cruise flight. The pilot was not injured. The airplane sustained substantial damage to the vertical stabilizer and rudder. The aircraft was registered to Aardvark Aircraft Acquisition LLC and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which was not on a flight plan. The flight originated from the North Omaha Airport (3NO), Omaha, Nebraska, about 1125 and was destined for the Rosecrans Memorial Airport (STJ), St Joseph, Missouri.The pilot reported that after climbing to cruise altitude and leaning the engine he noted an unusual engine vibration. He responded by enriching the fuel mixture slightly above normal and the vibration seemed better. After descending and increasing power to level off, the engine vibration became "much worse", and he elected to perform an off-airport precautionary landing. He stated that the landing was normal but during the landing roll, the main landing gear "dug in" and the airplane nosed over.

Postaccident examination of the airplane did not reveal any preimpact anomalies. The engine fuel servo, flow divider and nozzles were sent to the manufacturer's facility for testing under the direct supervision of NTSB investigators. The flow divider was tested and met all production test standards. The fuel nozzles were not flow tested but did not have any evidence of obstruction. The fuel servo was tested on the manufacturer's flow bench. The measured fuel flow rates were about 1.5 pounds per hour (1/4 gallon per hour) leaner than specified service limits.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN15LA170